Time-domain numerical simulation of a flow-impedance tube

Ozyoruk Y., Long L., Jones M.

JOURNAL OF COMPUTATIONAL PHYSICS, cilt.146, sa.1, ss.29-57, 1998 (SCI-Expanded) identifier identifier

  • Yayın Türü: Makale / Tam Makale
  • Cilt numarası: 146 Sayı: 1
  • Basım Tarihi: 1998
  • Doi Numarası: 10.1006/jcph.1998.5919
  • Dergi Adı: JOURNAL OF COMPUTATIONAL PHYSICS
  • Derginin Tarandığı İndeksler: Science Citation Index Expanded (SCI-EXPANDED), Scopus
  • Sayfa Sayıları: ss.29-57
  • Anahtar Kelimeler: flow-impedance tube, computational aeroacoustics, impedance conditions, z-transforms, nonreflecting boundary conditions, finite difference, COMPUTATIONAL AEROACOUSTICS, BOUNDARY-CONDITIONS, SOUND
  • Orta Doğu Teknik Üniversitesi Adresli: Evet

Özet

An efficient method has been developed for. the application of the surface acoustic impedance condition in time-domain solutions of aeroacoustic problems, such as the broadband-frequency simulation of a flow-impedance tube, The basis for this method is the standard impedance condition stated in the frequency domain as the particle displacement continuity equation. The development of the time-domain impedance condition follows the relations among the frequency. z-, and discrete-time domains and a rational function representation of the impedance in the z-domain. The resultant impedance condition consists of finite, infinite-impulse-response type, digital filter operations in the time domain, which is very suitable to computational aeroacoustics algorithms. This paper describes the present approach and discusses the time-domain numerical simulations of the NASA Langley how-impedance tube with a constant depth ceramic tubular liner. Both single and broadband-frequency simulations are performed. Excellent agreement is shown with experimental data at various frequencies and flow conditions. (C) 1998 Academic Press.